Accession Number : ADA293027
Title : High Temperature Oxidation-Resistant Materials. Phase 2.
Descriptive Note : Final rept. May 87-Aug 90,
Corporate Author : ULTRAMET PACOIMA CA
Personal Author(s) : Tuffias, Robert H. ; Melden, G. J. ; Harding, John T.
PDF Url : ADA293027
Report Date : MAR 1991
Pagination or Media Count : 94
Abstract : The objective of this project was to advance the state of the art in materials and processes for the fabrication of bipropellant chemical rocket thrust chambers. The results of the effort included the demonstration of materials and processes that permit thrust chamber operation at 2200 deg C (4000 deg F) for tens of hours, providing a 20-second increase in specific impulse; demonstration of process scaleup, from 5-lb(sub f) (22-N) to 100-lb(sub f) (445-N) chamber size; and development and characterization of the process to permit application of this technology to satellite and/or spacecraft propulsion systems. jg
Descriptors : *MATERIALS, *HIGH TEMPERATURE, *OXIDATION RESISTANCE, SPACECRAFT, COMPOSITE MATERIALS, ARTIFICIAL SATELLITES, SPECIFIC IMPULSE, THRUST CHAMBERS, BIPROPELLANTS, SPACE PROPULSION.
Subject Categories : Laminates and Composite Materials
Distribution Statement : APPROVED FOR PUBLIC RELEASE